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排序方式: 共有141条查询结果,搜索用时 15 毫秒
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对H形截面钢构件绕强轴压弯的极限抗弯性能展开研究。基于经实验校准的非线性有限元模型,进行了不同翼缘宽厚比、腹板宽厚比及轴压比组配下的H形截面钢构件的单调压弯全过程的参数分析,并对破坏模式进行了机理分析。研究表明,翼缘与腹板存在明显的相关作用,而板件屈曲形式决定了极限状态的应力分布形式,因此计算极限承载力时应考虑板件相关作用。以极限状态的应力分布特点为基础,提出了考虑板件塑性阶段屈曲相关作用的有效塑性宽度法计算截面的极限抗弯承载力。经与实验及有限元极限承载力的比较,显示该方法能够准确预测H形截面压弯构件的极限承载力。 相似文献
33.
利用ABAQUS有限元软件,对SHPB作用下的夹芯板的变形特性进行了分析,将有限元计算结果和实验测量结果作对比。在冲击载荷时间历程内,着重从芯板的位移和应力以及应变这3个方面对芯板的后屈曲问题进行了分析,研究了夹芯板中弹塑性压缩波的传播过程,芯板在压缩波作用下的动力屈曲产生、传播特性,压缩波与屈曲变形的相互作用以及塑性后屈曲大变形的发展规律。 相似文献
34.
B. Bochenek 《Structural and Multidisciplinary Optimization》2003,25(5-6):423-435
A proposal of a new approach to the optimal design of structures under stability constraints is presented. It is shown that the standard problem of maximization of the instability load may be modified so as to obtain a specified post-critical behaviour of the designed structure. The modified optimal structure represents stable post-buckling behaviour either locally, that is, in the vicinity of the critical point, or for a specified range of generalized displacements. First, some rigid–elastic finite-degree-of-freedom models are optimized, giving an insight into the modified design problems. Then a classification of the new optimization problems is presented. Various forms of instability are taken into account and a broad selection of objective as well as constraint functions is proposed. Based on the presented classification and following the proposed optimization concept, detailed formulations of nonlinear problems of design for post-buckling behaviour are given. 相似文献
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J. S. KOO B. M. KWAK 《International journal for numerical methods in engineering》1996,39(7):1161-1180
A linear complementarity problem formulation combined with an arc-length method is presented for post-buckling analysis of geometrically non-linear structures with frictional contact constraints. The arc-length method with updated normal plane constraint is used to trace the equilibrium paths of the structures after limit points. Under the proportional loading assumption, the unknown load scale parameter used in the arc-length method is expressed in terms of contact forces, and eliminated to formulate as a linear complementarity problem. The unknown contact variables such as contact status and contact forces can be directly solved in this formulation without any ad hoc technique. Complicated non-linear buckling behaviours, such as snap-buckling, can be efficiently solved by the developed method, as shown by several buckling and post-buckling problems with frictional contact constraints. 相似文献
37.
研究了复合材料加筋板翼面结构稳定性问题,分析了加筋板在压缩和剪切等载荷作用下的稳定性安全裕度。利用计算复合材料加筋板屈曲及后屈曲承载能力的方法,验证复杂受载情况下结构的稳定性。验证对象是一个优化后的满足强度、刚度和工艺制造要求的复合材料机翼。该机翼在各种载荷工况下的内力分布情况由MSC.NASTRAN分析得到,通过本文提出的方法得到每块蒙皮的稳定性承载能力。然后给出复合材料层合板在复杂载荷下的屈曲及后屈曲安全裕度的计算准则,验证优化后的机翼加筋板是否满足稳定性设计要求。该方法可作为约束集成到结构优化系统平台中。 相似文献
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39.
Nonlinear thermomechanical post-buckling of an imperfect functionally graded material (FGM) circular plate, subjected to both mechanical load and transversely non-uniform temperature rise, is presented. The material properties of FGM plates are assumed to be graded in the thickness direction according to a simple power law distribution in terms of the volume fractions of the constituents. Based on von Kármán's plate theory, equilibrium equations governing a large axi-symmetric deformation of the FGM circular plate under thermomechanical loads are derived. In the analysis, the geometric imperfections of the plate are taken into account. By using a shooting method the nonlinear ordinary differential equations with immovably clamped boundary conditions are solved numerically. Responses for the nonlinear thermomechanical post-buckling responses of the FGM plate are obtained. Numerical examples are presented that relate to the performances of perfect and imperfect, homogenous and graded plates. Characteristic curves of the post-buckling deformation of the imperfect FGM circular plate varying with thermal loads, imperfection parameters and volume fraction index are plotted. And then effects of the load parameters, materials constitution, and the geometric imperfection of the plate on the deformation are discussed in detail. 相似文献
40.
中国现行钢结构规范(规程)与美国ASD规范的主要限值 总被引:3,自引:0,他引:3
通过比较现行中、美两国的钢结构设计规范、规程中对受压杆件的长细比、翼缘宽厚比、腹板高厚比的极限值规定,阐述两国规范、规程中的差异和近似之处。 相似文献